USD950467S1 - Airplane - Google Patents
Airplane Download PDFInfo
- Publication number
- USD950467S1 USD950467S1 US29/729,612 US202029729612F USD950467S US D950467 S1 USD950467 S1 US D950467S1 US 202029729612 F US202029729612 F US 202029729612F US D950467 S USD950467 S US D950467S
- Authority
- US
- United States
- Prior art keywords
- airplane
- view
- broken lines
- design
- another perspective
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
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Description
The broken lines immediately adjacent the shaded areas represent the bounds of the claimed design while all other broken lines are directed to portions of the airplane and are for illustrative purposes only; the broken lines form no part of the claimed design.
Claims (1)
- The ornamental design for an airplane, as shown.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US29/729,612 USD950467S1 (en) | 2020-03-27 | 2020-03-27 | Airplane |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US29/729,612 USD950467S1 (en) | 2020-03-27 | 2020-03-27 | Airplane |
Publications (1)
Publication Number | Publication Date |
---|---|
USD950467S1 true USD950467S1 (en) | 2022-05-03 |
Family
ID=81328953
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US29/729,612 Active USD950467S1 (en) | 2020-03-27 | 2020-03-27 | Airplane |
Country Status (1)
Country | Link |
---|---|
US (1) | USD950467S1 (en) |
Citations (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
USD251721S (en) * | 1976-11-01 | 1979-05-01 | Stewart Anthony J | Aircraft |
USD257338S (en) * | 1978-11-09 | 1980-10-14 | Fairchild Industries, Inc. | Aircraft |
USD269176S (en) * | 1979-08-13 | 1983-05-31 | The Boeing Company | Supersonic airplane |
US4998689A (en) * | 1989-07-14 | 1991-03-12 | Rockwell International Corporation | 90 degree rotation aircraft wing |
USD317003S (en) * | 1989-10-25 | 1991-05-21 | Northrop Corporation | Aircraft |
US5062595A (en) * | 1990-04-26 | 1991-11-05 | University Of Southern California | Delta wing with lift enhancing flap |
USD370456S (en) * | 1995-04-04 | 1996-06-04 | The Boeing Company | Large, single deck, high wing airplane |
USD477561S1 (en) * | 2001-03-22 | 2003-07-22 | The Boeing Company | Supersonic aircraft |
US6698684B1 (en) * | 2002-01-30 | 2004-03-02 | Gulfstream Aerospace Corporation | Supersonic aircraft with spike for controlling and reducing sonic boom |
USD504654S1 (en) * | 2004-08-18 | 2005-05-03 | Northrop Grumman Corporation | Aircraft |
US20090206206A1 (en) * | 2006-10-18 | 2009-08-20 | Aerion Corporation | Highly efficient supersonic laminar flow wing |
US7624942B2 (en) * | 2006-06-20 | 2009-12-01 | United Technologies Corporation | Decoupled ducting for twin-engine reaction rotor drive |
US20110095137A1 (en) * | 2009-10-26 | 2011-04-28 | Aerion Corporation | Laminar flow wing optimized for supersonic cruise aircraft |
US8083171B2 (en) * | 2002-01-30 | 2011-12-27 | Gulfstream Aerospace Corporation | Supersonic aircraft for reducing sonic boom effects at ground level |
US8453961B2 (en) * | 2009-09-29 | 2013-06-04 | Richard H. Lugg | Supersonic aircraft with shockwave canceling aerodynamic configuration |
US10791657B1 (en) * | 2020-04-09 | 2020-09-29 | Aerion International Property Management Corporation | Composite aircraft structures with dividers for shielding and protecting cables and wires |
-
2020
- 2020-03-27 US US29/729,612 patent/USD950467S1/en active Active
Patent Citations (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
USD251721S (en) * | 1976-11-01 | 1979-05-01 | Stewart Anthony J | Aircraft |
USD257338S (en) * | 1978-11-09 | 1980-10-14 | Fairchild Industries, Inc. | Aircraft |
USD269176S (en) * | 1979-08-13 | 1983-05-31 | The Boeing Company | Supersonic airplane |
US4998689A (en) * | 1989-07-14 | 1991-03-12 | Rockwell International Corporation | 90 degree rotation aircraft wing |
USD317003S (en) * | 1989-10-25 | 1991-05-21 | Northrop Corporation | Aircraft |
US5062595A (en) * | 1990-04-26 | 1991-11-05 | University Of Southern California | Delta wing with lift enhancing flap |
USD370456S (en) * | 1995-04-04 | 1996-06-04 | The Boeing Company | Large, single deck, high wing airplane |
USD477561S1 (en) * | 2001-03-22 | 2003-07-22 | The Boeing Company | Supersonic aircraft |
US6698684B1 (en) * | 2002-01-30 | 2004-03-02 | Gulfstream Aerospace Corporation | Supersonic aircraft with spike for controlling and reducing sonic boom |
US8083171B2 (en) * | 2002-01-30 | 2011-12-27 | Gulfstream Aerospace Corporation | Supersonic aircraft for reducing sonic boom effects at ground level |
USD504654S1 (en) * | 2004-08-18 | 2005-05-03 | Northrop Grumman Corporation | Aircraft |
US7624942B2 (en) * | 2006-06-20 | 2009-12-01 | United Technologies Corporation | Decoupled ducting for twin-engine reaction rotor drive |
US20090206206A1 (en) * | 2006-10-18 | 2009-08-20 | Aerion Corporation | Highly efficient supersonic laminar flow wing |
US8453961B2 (en) * | 2009-09-29 | 2013-06-04 | Richard H. Lugg | Supersonic aircraft with shockwave canceling aerodynamic configuration |
US20110095137A1 (en) * | 2009-10-26 | 2011-04-28 | Aerion Corporation | Laminar flow wing optimized for supersonic cruise aircraft |
US10791657B1 (en) * | 2020-04-09 | 2020-09-29 | Aerion International Property Management Corporation | Composite aircraft structures with dividers for shielding and protecting cables and wires |
Non-Patent Citations (1)
Title |
---|
Supersonic Flight. by Aviation Internation News on YouTube. dated Jun. 2, 2021. found online [Jun. 30, 2021] https://www.youtube.com/watch ?v=X6NIGw_Cd-Q. * |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FEPP | Fee payment procedure |
Free format text: ENTITY STATUS SET TO UNDISCOUNTED (ORIGINAL EVENT CODE: BIG.); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY |